The grid embedding scheme is used to solve the whole flowfields around the combined configuration of the Hope, H-II rocket and rocket booster designed by the National Space Development Agency (NASDA). Three computational grids are overlapped with each other and the solutions are combined by interpolation at the boundaries. The Harten type Total Variation Diminishing (TVD) scheme is used to solve the Euler equations for hypersonic flow from M = 1.3 to 2.5, and it is shown the results of numerical simulation using the present methods are reasonable.
Numerical Simulations of Flow around a Body of Complex Configurations
1989
6 pages
Report
Keine Angabe
Englisch
Spacecraft Trajectories & Flight Mechanics , Rocket Engines & Motors , Aerodynamics , Fluid Mechanics , Aerodynamic configurations , Aerospace planes , Booster rocket engines , Computational fluid dynamics , Computational grids , Flow distribution , Hypersonic flow , Interpolation , Tvd schemes , Computerized simulation , Differential equations , Foreign technology
Hybrid RANS/LES Simulations for Flow Around Two Turret Configurations
British Library Conference Proceedings | 2008
|Scattering Simulations of Complex Configurations
British Library Conference Proceedings | 1997
|Computation of Viscous Flow Around Propeller-Body Configurations: Series 60 CB
Online Contents | 1994
|Scattering simulations of complex configurations
AIAA | 1997
|